Return-Path: Received: from imo-r06.mail.aol.com ([152.163.225.6]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Tue, 17 Oct 2000 08:13:31 -0400 Received: from CasaDeHate@aol.com by imo-r06.mx.aol.com (mail_out_v28.31.) id k.7b.aed48ab (4317) for ; Tue, 17 Oct 2000 08:20:43 -0400 (EDT) From: CasaDeHate@aol.com Message-ID: <7b.aed48ab.271d9e1b@aol.com> Date: Tue, 17 Oct 2000 08:20:43 EDT Subject: LIV Static Port Location To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> John Barrett etal: << I removed a 1 5/8" circle of inner graphite and honeycomb 4 inches behind the bulkhead that the Hydraulic pack attaches to and about 3/4" below the joint for the upper fuselage. Did this on both sides. Mark Mahnke at Lancair confirmed the position. >> I've found a great variance in the IAS using this location, the curvature of the fuselage seems to cause a lower pressure area aft of the baggage door, resulting in a lower IAS. This of course can only be verified, once finished, with some speed runs based against the GPS. Mike >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>